CL, CD at different AoA, Pressure Graph and Aerodynamics efficiency.
At forward inclination 1-5 degree & same for backward.
tsite
May 7, 2021, 12:15pm
2
Hi there, this is Fillia. If you need help with a project, please also share the link and more details
Best regards,
Fillia
Yes, Am trying to perform analysis of Multiplane. where i need to find out CL & CD at different AoA, Pressure Graph and Aerodynamics Efficiency also. where AoA is varying from 1-5 degree forward and backward.
tsite
May 7, 2021, 12:43pm
4
Alright, then have a look at the following tutorials and pages:
In this step-by-step tutorial, you will learn how to setup and post-process a compressible simulation around a wing. Join SimScale today!
Est. reading time: 24 minutes
This tutorial shows how a compressible simulation of a golf ball, using the k-omega SST turbulence model can be created, and then visualized.
Est. reading time: 20 minutes
In this article, you will learn to analyze the pitch, lift, and drag coefficients in an external aerodynamics simulation using SimScale.
Est. reading time: 4 minutes
In this documentation page, you will find information about how to set up forces and moments result controls in SimScale. Join us today!
Est. reading time: 6 minutes
You can use your own model for the simulation by following this CAD preparation& Upload guide:
Cheers!